Application of after-burning between high and low turbines to improve performance of two-spool turbofan engine

Shao Jun Qi; Yuan Hu Cai; Zhan Xue Wang; Ai Xue Ge

Application of after-burning between high and low turbines to improve performance of two-spool turbofan engine

Shao Jun Qi
, Yuan Hu Cai
, Zhan Xue Wang
, Ai Xue Ge

动力与能源学院

Fourth Inst.
Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 文章 › 同行评审

2 引用（Scopus）

摘要

On the basis of the thermodynamics model of two-spool turbofan engine, the performance of two-spool turbofan engine was improved by after-burning between high and low turbines. Effects of after-burning between high and low turbines on altitude, velocity and rotational speed characters were studied. The results show that the thrust is obviously increased and SFC maintained on basic level or decreased after adopting the after-burning between high and low turbines.

源语言	英语
页（从-至）	453-456
页数	4
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	23
期	6
出版状态	已出版 - 12月 2002

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引用此

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title = "Application of after-burning between high and low turbines to improve performance of two-spool turbofan engine",

abstract = "On the basis of the thermodynamics model of two-spool turbofan engine, the performance of two-spool turbofan engine was improved by after-burning between high and low turbines. Effects of after-burning between high and low turbines on altitude, velocity and rotational speed characters were studied. The results show that the thrust is obviously increased and SFC maintained on basic level or decreased after adopting the after-burning between high and low turbines.",

keywords = "Afterburning, Performance, Turbine, Turbofan engine",

author = "Qi, \{Shao Jun\} and Cai, \{Yuan Hu\} and Wang, \{Zhan Xue\} and Ge, \{Ai Xue\}",

year = "2002",

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T1 - Application of after-burning between high and low turbines to improve performance of two-spool turbofan engine

AU - Qi, Shao Jun

AU - Cai, Yuan Hu

AU - Wang, Zhan Xue

AU - Ge, Ai Xue

PY - 2002/12

Y1 - 2002/12

N2 - On the basis of the thermodynamics model of two-spool turbofan engine, the performance of two-spool turbofan engine was improved by after-burning between high and low turbines. Effects of after-burning between high and low turbines on altitude, velocity and rotational speed characters were studied. The results show that the thrust is obviously increased and SFC maintained on basic level or decreased after adopting the after-burning between high and low turbines.

AB - On the basis of the thermodynamics model of two-spool turbofan engine, the performance of two-spool turbofan engine was improved by after-burning between high and low turbines. Effects of after-burning between high and low turbines on altitude, velocity and rotational speed characters were studied. The results show that the thrust is obviously increased and SFC maintained on basic level or decreased after adopting the after-burning between high and low turbines.

KW - Afterburning

KW - Performance

KW - Turbine

KW - Turbofan engine

UR - https://www.scopus.com/pages/publications/0036978437

M3 - 文章

AN - SCOPUS:0036978437

SN - 1001-4055

VL - 23

SP - 453

EP - 456

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 6

ER -

Application of after-burning between high and low turbines to improve performance of two-spool turbofan engine

摘要

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